{"created":"2023-06-20T15:13:22.792379+00:00","id":43312,"links":{},"metadata":{"_buckets":{"deposit":"061874e6-677d-4271-bcd1-5a74fc686e80"},"_deposit":{"created_by":1,"id":"43312","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43312"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043312","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463142","463147","463140","463141","463146","463145","463144","463143"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Comparison with Computation Using Panel Method and Wind Tunnel Test Around Transonic Complete Aircraft"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"150","bibliographicPageStart":"141","bibliographicVolumeNumber":"9","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory SP-9","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The rapid progress of the computational aerodynamics enables us to analyze airflow with viscous calculation instead of with invisid one. In two-dimensional application, we have already validated its effectiveness in comparison with wind tunnel testing and put it into practical stage. In three-dimensional application, the wing-body configulation has been also done. This paper presents a validative discussion of the panel method toward the analysis about the complete aircraft, including the calculation of the sting interference, which is indispensable to wind tunnel testing. The results indicate that the panel method is valid in the subsonic region and that the sting makes up wash flow.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0009021","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-9","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業株式会社"},{"subitem_text_value":"三菱重工業株式会社"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"日本航空機開発協会"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮川, 淳一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳沢, 三憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 完一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyakawa, Jun-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagisawa, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Amano, Kan-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0009021.pdf","filesize":[{"value":"1.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0009021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43312/files/nalsp0009021.pdf"},"version_id":"4ea1ff42-826d-4675-ae7c-26eea248cf44"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"遷音速全機形状まわりのパネル法計算と風洞試験の比較","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速全機形状まわりのパネル法計算と風洞試験の比較"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43312","relation_version_is_last":true,"title":["遷音速全機形状まわりのパネル法計算と風洞試験の比較"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:17:40.697507+00:00"}